Motor-kite flying-machine.



G. w, SCHULTZ. v MOTOR KITE FLYING MAGHINE.- APPLICATION FILED D3014, 1907. 1,043,147, 1 Patented Nov. 5, 1912.

6 SHEBTSSHEET 1.

' 6501 e WSMZ.

e. W. SCHULTZ. MOTOR KITE FLYING MACHINE.

APPLICATION FILED 11150.14, 1907.

Patented Nov; 5, 1912.

6 SHEETS-SHEET 2.

G. W. SCHULTZ. MOTOR KITE FLYING MACHINE.

I APPLICATION FILED 1239.14, 1907. 1,043,, 147.

' Patented Nov. 5,1912.

6 SHEETS-SHEET 3 G. W. SCHULTZ. MOTOR KITE FLYING MACHINE.

APPLICATION FILED DBG.14, 1907.

1,043, 147., Patented Nov. 5, 1.912.

6 SHEETSSHEBT 4.

G W. $CIIULTZ.

MOTOR KLTE FLYING MACHINE.

APPLICATION FILED DEC. 14, 1007.

Patented Nov. 5, i912.

6 SHEETSSHEBT 5 G. W'. SCHULTZ.

MOTOR KITE FLYING MAGHINE. APPLICATION rum) 014, 1907.

' l wjiy I Patented Nov. 5, 1912.

6 BHBETSSHEET G.

UNITED STATES PATENT OFFICE.

GEORGE W. SCHULTZ, WAYNE, PENNSYLVANIA.

MOTOB-KITE FLYING-MACHINE.

Specification of Letters men.

Patented Nov. 5,1912.

Application filed December 14, 1907. Serial No. 406,440.

To all whom it nay concern:

' lie it knownthat I, GEORGE W. SCHULTZ, a citizen of the United States, residing in \Yayne, Pennsylvania, have invented certain Improvements in Motor Kite Flying -Machines, of which the following is a specification.

(me object of my invention is to provide a tlying' maehine of the aeroplane or heavierthan-air type, which shall be capable of sustaining itself in the air, together with one or more passengers and material to betrans ported. I I.

It is further desired to provide such a'lnachine with relatively simple'and at thesame controlling its movements after it has left the ground.

Another ob ect of the invention is to pro-- vide a flying n'iacl'nne having the above noted characteristics, wlthineans whereby I its equilibrium is maintained in the air and it can be more easily controlled as regards its upward, downward and sidewise movements than has hitherto beenpossible.

A further object of the invention is the generation and utilization of centrifugal force for increasing the stability of themaehine on its natural center of gravity While in the air. I

I also desire to provide a machine, which while beingicapable of sustaining and propelling itself in any direction through the air shall also be capable of operation upon land or water. I

These objects and other advantageous-ends 1 Secure as hereinafter set forth, reference being had to the accompanying drawings,

in which Figure 1, is a front elevation of one form of my invention; Figs. 2 and 3, are respec-.

tively a plan and a side ,elevation of the machine shown in Fig. 1; the upper aeroplane being omitted from the former figure; Figs. 4 and 5 are respectively a plan and,a side elevation of the rudders and their controlling mechanism; F ig. (5, is a side elevation of a modified construction of the rudders; Fig. 7, is a plan of a modified formof my 'flying machine, illustrating the application of the general principles of my invention to another arrangement of parts; Fig. 8', is a front elevation of the device shown in Fig. 7 Fig. 9, is a diagrammatic end elevation of a machine having a special form of side aeroplanes or wings; Fig. 10, is a side elevation of the device for insuring lateral stability of high speed machines having relatively narrow side wings.

In the above drawings an and a represent three upright frames braced together in any suitable manner, the first and last of these being extended as indicated at a in Fig. 1, to provide fot the attachment of a pair of hollow pointed cylinders B and B, extending longitudinally of the machine and pnadejo-ft' relatively light-sheet material. u'h

zilly metal, so to be water and air tight. ,Each of these extensibns a of the frame is provided with a portion a constructed to semeas'the axle of a wheel a whereby the "machine may be supported so as to'be capa ble of operation as a road vehicle. Eirtcnding between and connecting the frames are two aeroplanes C and D of a kite shape form, the latter being mounted at the top of thestructurejon the frames a, a and a and being pivoted or hinged to the last frame. The second of these aeroplanes indicated at C is placed approximately midway between the plane D and the bottom of the machine, and is preferably, thoughnot necessarily, of less length then said plane with which it is parallel. This top plane D has extending downwardly from its under side a pair of'cellular structures cl and d which, in the present instance, are ii rjtlie form of open ended triangular prismsttnd may be made in the manner common in the construction of box kites, cellular, superposed or 'plain kites without departing from my in vention. The planes C and l) are provided with square openings in their centers as indicated in Fig. 2, and would fly as a type of cellular kite if sent up in the usual way by a cord. The openings being inthe center allow for the exit of compressed air as the machine is descending, thereby preventing gyration and causing it to act as a parachute in case of failure of the motive power in mid air. Under operating conditions the machine would gravitate vertically or spirally to the earth, thus assuring safety and freedom from violentshock on alighting.

The structures d and d, as well as the planes (1 and. D, with the wings and the.

may be possible to employ thin sheet metal attached to the frames of the aeroplanes, etc, in any suitable manner.

The aeroplane D is preferably attached to its SllPPOItlllg framework a by a trans- 'ersel y extending hinge or hinges (1 so that itmay be turned on a transverse axis to elevate its front edge to a predetermined exic With this idea in View I provide the port on of the plane with tubular es (Z filling the upright members of the M3130, which have collars a to prevent iiimvnward moveinent'of saidfrontportion elow the horizontal and also heads a to the possible elevation thereof. The hung and lowering of the front edge is ac iplished by means of a rod cl extending .iwnwardly to point adjacent to the platin and constructed to be hooked or otherise attached to a. fixed portion to maintain e aeroplane B in its normal position under running conditions.

l lxtending transversely of the machine, preferably between thetwo frames (1. and c d at a point about midway between the ones C and D, is a framework E, shown .-th in full and in dotted lines in Fig. 1, hich includes two relatively long parallel bars 6 having at their ends kiteshaped planes 6' designed to serve as wings. Each ported.

of said Wing planes has projecting downwardly from its under side a prismatic cellular structure a open at the ends and on tending parallel w th the general line of. the machine; there being preferably though not necessarily rectangular openings through the central parts of these planes as shown. [is indicated in connection with the structures and (5 of the plane D, any other form of box, cellular, plain kite or wing shaped construction. may be substituted for these aeroplanes as desired.

The framework E is mounted and balenced upon a horizontal, longitudinally ex" tending shaft 6 carried in suitable bearings and movable therein. to a limited extent as a horizontal axis in order to place the planes 6 at an angle to the planes of the structures C and D.

Mounted just above the hollow floats B and B is a. platform F extending between the frames a and d and serving for the support of an operator, the motor or engine, and any supplies or apparatus to be trans- Between this platform and the pland (l is mounted a longitudinally extend-- ing rudder shaft G which, as illustrated in Figs. 1 to 3 inclusive, is mounted in hearings on the framework of the machine and carries at its forward end a plane g provided with a transverse spindle g movahly carried by said rudder shaft so asto be capable of being moved to be at any desired angle relatively to the fixed planes C and D. This rudder shaft projects at the front of the machine, while similarly carried on the rudder shaft G at the rear of the machine is a second rudder plane 9 which, like the first, has a transverse spindle 1, so that it also may be brought to any desired angle relatively to the plane C. For the purpose of controlling the position of these rudder planes and moving them at will. l provide upon the front spindle y a pulley wheel and upon the rear spindle g a pulley wheel g operativcly connecting said pulley wheels by a rope or.cable g, extending in the present instance through the rudder shaft, which is made tubular for the purpose. At some convenient point where the rudder shaft passes over the platforni l", I: provide in it a longitudinally extending slot having anumher of side notches To one run of the cable 9 l fix an operating handle j which projects through said slotand provide this with any desired form of spring latch operated by an auxiliary handle 7' This latter is capable of enterin r any of the notches j, and by means of this handle tnc cable may be moved to turn the pulley wheels and g and thereby alter the angles of the front and rear rudder planes.

Upon the rudder shaft G is mounted a sprocket Wheel 9 provided with any desired form ofclutch 9 whereby it may be operatively connected to or disconnected from said shaft at will and there is also fixed. to said shaft an operating handle 5 whereby it may be turned in its hearings to bring the rudder planes into such positions that their spindles are at right angles to the plane C. I. also mount a sprocket wheel 0 upon the shaft- 0 which carries the wing frame E and connect these two sprocket wheels by a chain 0' so that when desired the wing frame may be turned at any desired angle, either in connection with on independently of the rudder shaft and the rudder planes, depend ing on whether or not the clutch y is thrown into action.

The engine H for driving the machine is mounted in any suitable manner upon the platform F of the machine, preferably below the rudder shaft G and it is so placed that its main shaft 72 extends longitudinally of the machine to a bearing c on the frame. This shaft has mounted on its end a double grooved pulley It and ncludes a clutch h whereby said pulley and the parts actuated therefrom may be disconnected at will from the engine. Turned in opposite directions from the pulley through any desired belts or chains are a pair of propellers h which serve to drive the machine regardless of whether it operates upon air, water or land.

The front end of the engine shaft has a disk fly-wheel 71. provided with teeth engaging gear wheels h on shafts If so as to turn two heavy fly wheels 1. mounted thereon in opposite directions; the said wheels thus constituting a double gyroscope. These shafts are mounted in bearings formed in frames h rigidly mounted upon a single frame it, rotatably carried on the shaft h as an axi so that this latter frame may 0s rillate in a vertical plane but not otherwise. The axles or shafts k are extended out under the side wings of the machine and in orde lifo limit their possible oscillation in an-wticollplane I mount upon the side members of the main frame of 'the machine, stops u." so placed that under predetermined conditions they will engage said shafts. From each end or other suitable point upon the frame E, I mount a downwardly extending.

rod or:barip haitingl at its lower end a loop or slotted portion 3)" through which extends one of theshafts ii; the arrangement being 1 such that in the event of the frame turning: on its axis more than a predetermined amount from its normal position parallel with said shafts, one or the other of the slotted ends [1 of the rod will engage its 0 shaft. The ends of the shafts if are proridcd with screhs or fans it hereby under operating conditions air may be drawn in toward the center of the machine or lnrusted therefrom as may be found con- ,9 ducive to best results under operating condiaious. As a result of such action a considerable volume of air is or may be drawn in mulcr the central parts ofthe aeroplane so as to assist in buoying it up and at the same time materially add to its stability.

' it is tobe noted that the belts or chains 7a?" are so arranged that the propellers 72- are (ll'lVGIl in opposite directions, it beinguudcrstood that their design is such that 40 und +hese conditions theyact together to propel the machine either forward or backward. i

All indicated at k in Fig. 2, I may place any suitable form of clutch between the,

main shaft of the engine and the propellers so that these may be thrown into and out of action without interfering with the opera lion of the fly heels of the gyro-scope, \rhi 'h underwvorking conditions are at all limos in revolution. v I

Hue object of the liy Wheels mounted as lH -.\"ll, is to produce the effect of a double *"f shall be capable of autothe equilibrium of "ins the action of Wind Pl'thrllll j. 111;; to tilt it laterally, tic

movement of the operator or any GU16! lorrc tending to deflect it from its proper posit ion.

W it will be understood that the main frame of the machine Well as theframes of the various planes, wings, sails, etc, are of any light, strong construction properlybraced :ic members usually formed of p ano wire. 1?? In order to use the machine above described, I first run it along a road or other level tract and for this purpose drive it by means of the engine ll. This. as will be understood, operates the fans or propellers /1. at a high speed and as long as the Various planes and wings of the machine are horizontal, provides no lifting force. 11. how ever, the front and rear rudders be set at. some such angle as indicated in Fig.5, and the top plane D be moved to a position'with its front portion raised, the machineimme- Y diately tends to rise owing to the upwardly acting component of the force resulting from the air striking the inclined surfaces; of the rudders and the said plane D. After the machine has left the. ground the continuous operation of the propellers still tends to drive it forward, While the level at which it moves may be determined by vary: ing the angle of the rudders either with or 5 Without an adjustment of the aeroplane D. By means of the handle the Wings 6 of the fra rneflfi may he set at any desired angle to the aeroplane l and C so as to overcome the effects of any air currents tending to throw the nmchine out of its proper position. These side Wings, which may, as previously noted be adjusted simultaneously Wii'lrthe rudders, have the tune tions of the Wings of a, bird in balancing or steering, While similarly, the front and rear rudders act in the same manner as do the head and tail of a bird to determine th leyel of flight. By means of the handle 7' the rudderplanes are set at any desired angle .100 as determined by the longitudinal position. of said handle in theslot of the rudder shaft; it being held in any adjusted position by means of the engagement of its spring latch with the notches j.

In the event of the flying machine being tilted or displaced mor'e than a predeterHv mined amount from its normal level, one or the other ofthe slotted ends 7) of the rods 7) engages one ofthe shafts h and inasmuch asthe rotation of the fly Wheels tends to maintain these shafts at all times parallel to V themselves, the side wings and the parts attached to'thcm are prevented from moving at an abnormal extent beyond their safe positions. Similarly, should the machine as a whole be tilted or should it turn on a horizontal axis so to be in danger of upsetting, one of the stops a would engage the shaft h adjacent to it and effectually prevent- -such dangerous movement of the machine. I am, therefore, enabled to maintain my machine on a substantially level keel,

and if desired, in place of the four vehicle wheels at its sides as illustratedin Figs. 1, 2, etc., I may provide two or more wheels inthe central plane of the machine, inasmuch as its balance is automatically maintained by the gyroscopic apparatus above described.

The various cellular structures d, d and 1% of the Wing d not in the manner and perform the functions eharacteristic of cellular or box-kites and materially add to the lilting and steering power of the ma hine. If desired the wings or wing planes may be constructed as shown in Fl 0, so that there is at each end trame. E a plurality of superpos d double or multiple planes c held together and to said frame in any suitable manner.

Owing to the fact that the engine, opera.- to and wheels are) carried upon the lower halt ot the machine, the center oi gravity of the structure as a whole is considerably below its center, with the'result that its sta bility under operating conditions is exceptiouall) high.

is is obvious. the lloats l3 and i3 keep the ma hine from sinking should it alight on the surface oi water. while the propellers ;-.('l'\'(3 to move the machine regardless of whether it operates in the air, water or upon the surface of the earth.

In case it. should be desired to have the rudder controlling cable outside the rudder shalt. (i this may be constructed in the manner illustra ed in Fig. (3, with the cable extending in straight lines directly between the wheels 7" and In any case the rudder planes are {noperly trussed or braced so to pit-vent any distortion which might otherwi e war in a strong wind.

In Fig. '7 and 8, i have illustrated 'a inodilird form of my machine in which its various parts have been made to more closelv conform to the analogous parts of a bird;

certain of its various surfaces or aeroplanes being cancam-convex in contradistinction to the flat aeroplanes employed in the motor kite term of my invention. For this purpose the. planes 0 of the wing structures are given concave-convex forms more nearly approaching those of a birds wlng, as indicared at c though the front; and rear rud-' (101' planes 9' and g" are perfectly flat surfaces. The lower plane C is replaced by a hollow sheet metal body C blunt. pointed at its forward and more sharply pointed at. the rear, which under operative conditions is intended to receive passengers, material to be transported, etc. In spiteot these changes,

however, it is obvioiis that this form of the invention depends for its operation upon the same principles as those characterizing that: form of my device illustrated in Figs. 1 to 4 inclusive, there being as in this other form a top plane D, which, however, is of a concavo-convex construction.

In the motor kite' flying machine above described the object is to construct a relatively slow speed but sate device designed to carry one man and to'move with its planes at a considerable angle of incidence to the air. The side or transverse spread of its Wings is preferably not greater than the total length of the machine and its fore and aft. rudders are placed a considerable dis-- tance apart. with the center of gravity relatively low, so that asa result the longitudinal stability easily under the c ntrol of the operator in case there should he encountered a sudden gust of wind coming from the front. When. however, it is desired to provide a machine capable of greater speed and having an increased weight. carrying capacity. such as that shown 'in t in'is. 7 and 8, em 'iloy relatively narrow wings of wide lateral expanse. raise the. center oi gravity nearly to the level of the wing plan and in order to v eem-e longitudinal stability at a. small angle oi incidence a necessary for rapid flight, place the t y wheels ot the gyroscope so that they normallv lie inJhorizootal planes. The truuuions tor the lly wheel frames are on the sides at the maehineso as to permit the axes of the fly wheels I" move only in a direction longitudinal witti the machine.

I claim:

1. The combination in a lying machine of an aeroplane, an engine. two tly wheels placed some distance apart oneon each side of the engine and driven thereby. and propellers also driven by said engine, said lly wheels being placed on axes at right angles to the axes of the propellers.

2. The combination in a flying n'uu'rhine of a frame. an :wroplane thereon. a driving motor. and a propeller or propellers act-uated thereby to force the machine l'orward, said aeroplane havinga central unobstructed opening and a transversely extending adjustable stru irturc mounted on said frame and having an aeroplane on each end.

3. The combimitionin a flying machine of a frame, an aeroplane thereon. a driving motor, and a propeller or prrmellersactuated thereby, a udder. with mechanism independent of said rudder for maintaining the stability ol. the machine, said aeroplane having an opening placed to also maintain its. stability during the descent of the machine, independently of said n'iechanism; and

.an adjustable transversely extending structure mounted on the frame and provided at each end with an aeroplane.

4. "lhe combination in a flying machine of a frame; propelling means; atransversely extending structure movably mounted on the frame; an aeroplane rigidly and permanently connected to each end of said structure; and means for adjusting the trans macaw the machine, an aeroplane at each endof said structure, a motor, and propelling.

connected to said frame and provided at each end with an aeroplane, \vith meansfor varying the position of'said frame to vary the angle of its aeroplane to the first aeroplane, i i

8. The combination in a flying machine of a supporting structure, an upper and a lower aeroplane attached thereto, propelling means, With a transversely extending frame mounted between said aeroplanes, said latter frame having at each end asupplementary aeroplane and being adjustable on an axis extending longitudinally of the machine.

The combination in a flying-machine of a supporting frame, an upper and a lower aeroplane attached thereto, propelling means, and a transversely extending frame mounted between said aeroplanes, said latter frame having at each end a supplementary aeroplane and being adjustable upon an extending longitudinally of the machine, each of said aeroplanes on the adjustable frame having attached to it a cellu lrite structure.

O. The combination in a flying machine frame, an aeroplane at the irojccn from its unapart and J r o the front and of the aeroplane, with their longitudinal axes i he median plane of the machine, and an adjustable lateral! y extending memtively placed her having plane on each side of the center of the machine.

11. The combination in a flying machine of a supporting frame, an aeroplane at the top theredf having projecting from its unside a cellular kite structure, with propelling means for said machine, and. a transversely extending structure provided at its ends with aeroplanes, each also provided with a cellular kite structure. l

12. The combination in a flying machine of alsupporting frame having an aeroplane, propelling means mounted on the frame, a

tubular slotted rudder shaft, two pulleyto it two through the slot in the rudder shaft, with a rudder connected to each of said Wheels so as to be movable therewith.

13. The combination of a supporting frame having a hollow float or floats, a motor, a propeller or propellers driven therefrom, one or more aeroplanes mounted above said propeller or propellers, and Wing structures projecting at each side of the frame, said structures including a transversely exteiziding frame having an aeroplane at each on 14. The combination of a supporting frame having a hollow float or floats, a motor, a propeller or propellers driven therefrom, one or'more aeroplanes mountedabo e the propeller or propellers, and wing structures at each side of. the frame having a framemounted to be adjustable on an axis extending longitudinally of the machine.

15. A flying machine consisting of a main frame, vehicle wheels mounted thereon, a motor, a propeller or propellers driven from the motor, an aeroplane mounted above the motor, means for raising at Will the front portion of said aeroplane relatively to the rest of the machine, with means consisting of headed projections fixed tn the frame for limiting the amount of such elevation of the front portion.

16. The combination with a flying. machine of a gyroscopic device, the same con sisting of two similar heavy rim fly Wheels mounted close together adjacent to the cen ter of gravity of the structure, means for rotating said wheels at relatively high but equal speeds in opposite directions, each Wheel having a separate supporting shaft extending outwardly, with a propeller on each shaft for producing side currents of air. 7

1.7. The combination in a flying machine of an acro 'ilane, a frame, a pair of shafts extending transversely of the machine beloiv the aeroplane, fly Wheels on said shafts, and means for turning the fly wheels inopposite directions.

18. The combination in a flying machine, of an aeroplane, a frame, shafts extending transversely of the machine below the aero' plane, fly Wheels on said shafts, means for turning the shafts, a longitudinally extending rudder shaft, a rudder or rudders mounted on said latter shaft, and propelling means for the machine.

19.111 a flying machine, the combination of a frame having attached to it an aeroplane, a transversely extending frame hav ing side Wings and so mounted upon said first frame that the latter may be free to and mechanism connecting said apparatus to the transverse frame to limit the turning thereof.

20. In a flying machine, the combination of a frame having attached to it an aeroplane; a laterally extending balancing device so mounted upon said first frame that the latter may be free to turn about a longitudinal axis, a motor carried by the ma chine; gyroscopic apparatus driven by the motor; and mechanism connecting said apparatus with the balancing device to limit the possible movement thereof.

21. The combination of a main frame having one or more aeroplanes, a motor mounted on the frame, roscopic apparatus driven by the motor including transversely extending shafts, said gyroscopic apparatus being pivotally mounted on an axis extending longitudinally of the machine, with stops on the frame placed to engage said shafts in the event of relative movement of the apparatus and frame beyond a predetermined amount.

22. The combination in a flying machine, of a frame, having one or more aeroplanes, a motor mounted on the frame, a propeller or propellers actuated therefrom, gyroscopic imam? 4 apparatus also driven by the motor and including a transversely extending shaft or shafts, a tan or fans carried by said shaft or shafts, and means whereby abnormal tilting of the frame is prevented by the gyroscopic apparatus.-

23. The combination in a flying machine of a frame having one or more aeroplanes; a motor mounted on the frame; a poopcller or propellers driven thereby; a transversely extending shaft or shafts having actuating means; a fan or fans on said shaft or shafts placed laterally beyond and outside 'of the line of said propeller or propellers to draw in air under the aeroplane or aeroplanes; and gyrosoopic stabilizing means operative on said shaft r shafts.

In testimony whereof I have. Slflltjrld, my name to this specification, in the tiresome of two subscribing witnesses.

GEORGE W. SCHULTZ.

Witnesses:

FRANK SMITH, C. R. KENNEDY. 

